Micromix fuel injection air nozzles
Known micromixers for fuel injection (e.g., in a gas turbine engine) experience early burning or have limited operability. Accordingly, a micromixer is disclosed that utilizes an air nozzle, in combination with one or more fuel jets, to produce short flames that minimize the emission of nitrogen oxides, while providing additional benefits, such as mechanical robustness, aerodynamic efficiency, resistance to flame damage, suitability for additive manufacturing, wider operating ranges, operation with a variety of gaseous fuels, and/or amenability to control using conventional mechanisms.
1. A micromixer comprising:
a main body that includes an air nozzle defining a flow path through the main body along a first axis in a downstream direction, the air nozzle comprising an outlet portion having an outlet at a downstream end of the air nozzle;
a step extending from the main body along the first axis, the step comprising a surface that extends in the downstream direction from the outlet of the air nozzle and is parallel to the first axis; and
a fuel supply that includes a fuel chamber, extending into and terminating in the step, and at least one fuel jet that provides fluid communication between the fuel chamber and an area downstream of the outlet, and extends through the surface of the step at a location downstream of the outlet.
2. The micromixer of claim 1 , wherein the air nozzle comprises:
an inlet portion that converges in the downstream direction; and
wherein the outlet portion is downstream from the inlet portion and diverges in the downstream direction.
3. The micromixer of claim 2 , wherein the air nozzle further comprises a throat portion between the inlet portion and the outlet portion.
4. The micromixer of claim 1 , wherein a cross-sectional area of the air nozzle, in a plane orthogonal to the first axis, decreases from an inlet of the air nozzle to the outlet of the air nozzle.
5. The micromixer of claim 1 , wherein a cross-sectional profile of the air nozzle, in a plane orthogonal to the first axis, is circular for at least a portion of the air nozzle.
6. The micromixer of claim 1 , wherein a cross-sectional profile of the air nozzle, in a plane orthogonal to the first axis, is rectangular for at least a portion of the air nozzle.
7. The micromixer of claim 1 , further comprising one or more additional fuel jets which connect the fuel chamber to the flow path.
8. The micromixer of claim 1 , wherein one of the at least one fuel jets is angled downstream, such that an end of the one fuel jet that is connected to the fuel chamber is upstream from an opposite end of the one fuel jet.
9. The micromixer of claim 1 , further comprising a second fuel supply that includes a second fuel chamber and one or more second fuel jets that provide fluid communication between the second fuel chamber and the flow path.
10. The micromixer of claim 1 , further comprising a turbulence-generating body at the outlet.